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October 12, 2010
Slide - 1
The First Moscow Solar System Symposium
“Luna Glob” and “Luna Resource” Missions
L.M.Zelenyi(1, V.V.Khartov(2 I.G.Mitrofanov(1 and A.A.Skalsky(1
1) Institute for Space Research 2) Lavochkin Association
October 12, 2010
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The First Moscow Solar System SymposiumLunar Exploration Neutron Detector Polar Map
North pole South pole
Lunar Exploration Neutron Detector (LEND) is one of the instruments aboard NASA’s Lunar Reconnaissance Orbiter (LRO). It is the first collimated neutron instrument to ever fly in space allowing it to achieve high spatial resolution for mapping neutron emission from the Moon. The map above shows neutrons count rate at the Moon’s poles, where a decrease of counts means higher content of hydrogen in regolith. Gray color and black contours represent surface relief and permanently shadowed regions. LEND is a contribution of the Russian Federation to the LRO mission developed under an Agreement between NASA and Roscosmos in Space Research Institute (IKI), Moscow.
October 12, 2010
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The First Moscow Solar System Symposium
LUNA-GLOB
Long-term Strategy: Successive Steps for Robotic Lunar Missions (2011 – 2020)
LUNA-RESOURCE
LUNA-LD-ROVER
LUNA-SR
October 12, 2010
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The First Moscow Solar System Symposium
October 12, 2010
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The First Moscow Solar System Symposium
Luna-Resource (Polar Lander)withChandrayaan-2 (India, Orbiter)
2013
Luna-GlobwithPolar Lander and Orbiter
2012
Mini-Rover (India)
October 12, 2010
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The First Moscow Solar System Symposium
Luna-Resource (Lander)withChandrayaan-2 (India, Orbiter)
2013
Luna-GlobwithLander and Orbiter
2012
Mini-Rover (India)
October 12, 2010
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The First Moscow Solar System Symposium
Landers configuration
Mini-Rover (India)
Drillingsystem
LUNA-GLOBLUNA-RESOURCE
ManipulatorManipulator
October 12, 2010
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The First Moscow Solar System Symposium
Main Scientific Tasks of Landers:
TASK 1: Investigation of composition of subsurface and processes of its formation at Lunar Poles (volatiles, H2O, layering, etc.)
TASK 2: Investigation of interaction between cosmic plasma and surfaceand processes of exosphere at Lunar Poles (solar wind, neutrals, dust)
Main Criteria for payload Selection
1) Correspondence to TASKS 1 or 2
2) High TDR Level > 6
October 12, 2010
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The First Moscow Solar System Symposium
Selected Scientific Payload of Landers of L-R and L-GInstrument Measurements/Operations Mass (kg) PI
Navigation
Radio-Beacon Radio signal with good stability 1.1 A.S.Kosov, IKI
Instruments for remote studies of regolith on Manipulator
TV for Field of Operations Imaging of Field of Operation with Pointing Capability
0.5 A.V.Bondarenko, IKI
LIS_IR IR spectra of minerals 1.0 O.I.Korablev, IKI
Instruments for analysis of regolith served by Manipulator
Gas analytic complex Analysis of volatiles content and isotopic ratios 10.4 M.V.Gerasimov, IKIand Vernadsky Institute
LASMA Laser mass-spectrometer 2.6 G.G.Managadze, IKI
Instruments for remote sensing
Optical Spectrometer-Imager Optical imaging of minerals with UF exitation 0.5 A.N.Lipatov
ADRON Active neutron and gamma-ray analysis of nuclei composition
6.7 I.G.Mitrofanov, IKI
Radiometer-Thermometer Measurements of temperature of subsurface regolith
0.5 D.P.Skulachev, IKI
Contact Thermometer Measurements of temperature of regolith on surface and in drilling hole (for L-G only)
0.4 L.P.Moskaleva, Vernadsky Institute
PmL Measurements of dust 1.5 G.G.Dolnikov, IKI
LINA and ARIES Measurements of plasma and neutrols 3.8 A.A.Skalsky and O.L.Vaisberg, IKI
Seismometry
SEISMO Measurements of seismic activity 1.0 A.B.Manukin, Institute of Physics of Earth
October 12, 2010
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The First Moscow Solar System Symposium
10
Radio-Beacon Transmitter
Two transmitters X and K band 0.2 Wt
Frequency stability 5 x 10-13 for <100 s or1 x 10-13 for <103 s
Flight prototype for Phobos-Soil-Returnmission
Science Task 1:
Study of internal motions of the Moon by the phase-referencing method with supportof ground radio telescopes for investigations of internal structure of the Moon
Science Task 2:
Study of relative motion between Lander and Orbiter of Lunar-Glob for investigation of lunar gravity field
Service Task:
To provide radio-beacon service for future landers and orbiters
October 12, 2010
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The First Moscow Solar System Symposium
LIS – Lunar IR Spectrometer
Spectral range 1.4 – 3.5 microns
Spectral resolution 15 – 25 nm
Field of View about 1, or 17 cm at 10 m
Science TASK 1:
Measurements of OH and H2O content in polar regolith on the surface and withina shallow subsurface
Science TASK 2:
Testing for daily variations of hydratation and for decay of hydratation after removing of the upper-most layer
spaceprototype
October 12, 2010
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The First Moscow Solar System Symposium
Gas Analytic Complex
- Thermal Differential Analyzer
- Gas Chromatograph
- Mass Spectrometer
Instrument for Phobos-Soil-Return, asprototype
Science TASK 1:
Measurements of volatiles in lunar regolith from the surface and within a shallow subsurface
Science TASK 2:
Testing for isotopic ratios of particular elements of volatiles in lunar regolith
October 12, 2010
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The First Moscow Solar System Symposium
LASMA – Laser Mass Analyzer
- Laser-evaporation system of testing samples
- Mass Spectrometer
Instrument for Phobos-Soil-Return, as prototype
Science TASK 1:
Measurements of volatiles in lunar regolith from the surface and within a shallow subsurface
Science TASK 2:
Testing for isotopc ratios of particular elements of volatiles in lunar regolith
October 12, 2010
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The First Moscow Solar System Symposium
Optical Spectrometer-Imager
Imaging of surface at three optical spectral bands
Photometry of surface at 9 narrow spectral bandsfrom 278 to1052 nm
UV-luminescent analysis
Science TASK 1:
Mineralogical composition of polar regolith and separate stones on the surface and withina shallow subsurface
Science/Service TASK 2:
Imaging of Field of Manipulator Operations in 3 optical spectral bands
October 12, 2010
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The First Moscow Solar System Symposium
ADRON
- Pulsing neutron generator to study composition of subsurface regolith
- Detector of post-pulse neutrons
- Detection of post-pulse gamma-rays
Instruments for Phobos-Soil-Return and NASA MSL, as prototype
Science TASK 1:
Measurements of neutron post-pulse emission to study content of hydrogen and layering structure of shallow subsurface
Science TASK 2:
Measurements of gamma-rays post-pulse emission to study composition of regolith and layering structure of shallow subsurface
October 12, 2010
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The First Moscow Solar System Symposium
Radiometer-Thermometer
- Measurements of radiation from subsurface at 2.5, 3.3 and 5.0 cm
- 1 meter depth temperature variation with 15 cm discreetness and accuracy about 1 degree
Instrument for Relict project is used, as prototype
Science TASK 1:
Measurements of diurnal and annual variations of subsurface temperature
Science TASK 2:
Measurements of complex dielectrical parameter of regolith
October 12, 2010
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The First Moscow Solar System Symposium
PmL – Dust Detector
- Measurements of impacts from dust grains with accuracy of 10-12 – 10-14 N sec
- Measurements of charge about -10-12 Qoulomb
Instrument for Phobos-Soil-Return mission is used, as prototype
Science TASK 1:
Measurements of flux, distribution of mass and distribution charge of lunar dust
Science TASK 2:
Detection of micro-meteorites and secondary particles of regolith
October 12, 2010
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The First Moscow Solar System Symposium
LINA – Detector of charge particles and neutrals
- Measurements of ions <40 amu of solar wind 10 eV – 15 keV - Measurements of neutral particles 1 – 56 amu with energy 10 eV – 3.2 keV
Instrument for Phobos-Soil-Return mission is used, as prototype
Science TASK 1:
Interaction of solar wind with lunar surface at poles
Science TASK 2:
Creation and transport of charged and neutral particles in lunar exosphere
October 12, 2010
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The First Moscow Solar System Symposium
ARIES – Panoramic energy-mass spectrometer of ions
- Measurements of ions 1 - 100 amu of solar wind 3 and exosphere 3 eV – 5 keV - Directional measurements of of impact particles 7.5 x 15
Instrument for Phobos-Soil-Return mission is used, as prototype
Science TASK 1:
Interaction of solar wind with lunar surface at poles
Science TASK 2:
Creation and transport of charged particles in lunar exosphere
October 12, 2010
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The First Moscow Solar System Symposium
Strategy and time of missions implementation (Landers)
2011 2012 2013 2014
Mass UThermal U
EU
QU
FU01, FU02, FU03
Baikonor for LUNA-GLOB
India for LUNA-RESOURCE
Flight Spare
Science Study Teams
October 12, 2010
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The First Moscow Solar System Symposium
FIRST ANNOUNCMENT
1st International Workshop “Landing site selection for Luna-Glob Lander”
Institute for Space ResearchMoscow
January 25 – 27, 2011
Goal of the 1st Workshop:Identification of the most interesting and safe landing sites candidates for Lander of “Luna-
Glob” Mission
Participation in the 1st Workshop:Co-investigators of “Luna-Glob” mission, participants of another lunar missions with intention
for cooperation, endorsed representatives of space agencies andspace science centers, authors of invited and contributed presentations
Program of the 1st Workshop:Concept of Lander – Engineering constrains for landing – investigations with
selected instruments of the Lander – coordination with another missions - presentations of landing sites candidates – definition of candidates list
Applications for participation with Abstracts of presentations should be submitted toIgor Mitrofanov ([email protected]) or Maxim Litvak ([email protected])
with deadline of October 17, 2010
Workshop Organizers: Academician Lev Zelenyi, Scientific Lead of “Luna-Glob” mission
Dr. Igor Mitrofanov, Mission Scientist of Lander of “Luna-Glob”
October 12, 2010
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The First Moscow Solar System Symposium
Luna-Resource (Lander)withChandrayaan-2 (India, Orbiter)
2013
Luna-GlobwithLander and Orbiter
2012
Mini-Rover (India)